As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BULGING AND PILLOWING SKIN AT BS 1085 THRU BS 1110 ALONG FASTENER ROWS AT STRINGER 17R THRU 19R ON EXTERNAL FUSELAGE. ACCOMPLISHED FUSELAGE SKIN REPAIR FROM BS 1085 TO BS 1110 BETWEEN STRINGER 17R AND 19R DUE TO CORROSION IAW MFG ENGINEERING RO. (MATERIAL USED 2024-T3 .090 INCHES, 86 INCHES X 38 INCHES.